Stability of hybrid airships
The mathematical model of a winged hybrid airship is developed for the analysis of its dynamic stability characteristics. A full set of nonlinear equations of motion of the hybrid airship is determined and adequate assumptions are made in order to apply any relevant computation and estimation method...
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| Format: | Monograph |
| Language: | English |
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s.n
2012
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| Online Access: | http://irep.iium.edu.my/36044/ http://irep.iium.edu.my/36044/ http://irep.iium.edu.my/36044/1/EDW_A12-610-1401.pdf |
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eprints |
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iium-360442015-05-13T08:13:13Z http://irep.iium.edu.my/36044/ Stability of hybrid airships Asrar, Waqar T Technology (General) T57 Applied mathematics. Quantitative methods. Operation research. System analysis TA329 Engineering mathematics. Engineering analysis The mathematical model of a winged hybrid airship is developed for the analysis of its dynamic stability characteristics. A full set of nonlinear equations of motion of the hybrid airship is determined and adequate assumptions are made in order to apply any relevant computation and estimation methods. The design of the hybrid airship is slightly modified to suit the demanding requirement of a complete and feasible mathematical model. Linearization is then performed under a chosen trim condition, and eigenvalue analysis is carried out to determine the general dynamic stability characteristics of the winged hybrid airship. The result shows that the hybrid airship possesses dynamic instability in longitudinal pitch motion and lateral-directional slow roll motion due to the strong coupling between the aerostatic lift from the buoyant gas and aerodynamic lift from the wing s.n 2012-12-10 Monograph NonPeerReviewed application/pdf en http://irep.iium.edu.my/36044/1/EDW_A12-610-1401.pdf Asrar, Waqar (2012) Stability of hybrid airships. Research Report. s.n, Kuala Lumpur. (Unpublished) EDW A12-610-1401 |
| repository_type |
Digital Repository |
| institution_category |
Local University |
| institution |
International Islamic University Malaysia |
| building |
IIUM Repository |
| collection |
Online Access |
| language |
English |
| topic |
T Technology (General) T57 Applied mathematics. Quantitative methods. Operation research. System analysis TA329 Engineering mathematics. Engineering analysis |
| spellingShingle |
T Technology (General) T57 Applied mathematics. Quantitative methods. Operation research. System analysis TA329 Engineering mathematics. Engineering analysis Asrar, Waqar Stability of hybrid airships |
| description |
The mathematical model of a winged hybrid airship is developed for the analysis of its dynamic stability characteristics. A full set of nonlinear equations of motion of the hybrid airship is determined and adequate assumptions are made in order to apply any relevant computation and estimation methods. The design of the hybrid airship is slightly modified to suit the demanding requirement of a complete and feasible mathematical model. Linearization is then performed under a chosen trim condition, and eigenvalue analysis is carried out to determine the general dynamic stability characteristics of the winged hybrid airship. The result shows that the hybrid airship possesses dynamic instability in longitudinal pitch motion and lateral-directional slow roll motion due to the strong coupling between the aerostatic lift from the buoyant gas and aerodynamic lift from the wing |
| format |
Monograph |
| author |
Asrar, Waqar |
| author_facet |
Asrar, Waqar |
| author_sort |
Asrar, Waqar |
| title |
Stability of hybrid airships |
| title_short |
Stability of hybrid airships |
| title_full |
Stability of hybrid airships |
| title_fullStr |
Stability of hybrid airships |
| title_full_unstemmed |
Stability of hybrid airships |
| title_sort |
stability of hybrid airships |
| publisher |
s.n |
| publishDate |
2012 |
| url |
http://irep.iium.edu.my/36044/ http://irep.iium.edu.my/36044/ http://irep.iium.edu.my/36044/1/EDW_A12-610-1401.pdf |
| first_indexed |
2023-09-18T20:51:37Z |
| last_indexed |
2023-09-18T20:51:37Z |
| _version_ |
1777410032228368384 |